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IMAGING ASSISTED GAS TURBINE ANTI-ICING SYSTEM

  • US 20160245178A1
  • Filed: 02/24/2015
  • Published: 08/25/2016
  • Est. Priority Date: 02/24/2015
  • Status: Active Grant
First Claim
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1. A method comprising:

  • receiving image data from a camera coupled to an air intake system of a gas turbine engine, wherein the image data corresponds to an air passage of the air intake system;

    comparing the received image data to reference image data of the air intake system; and

    generating an icing notification based at least in part on the comparison when a difference between the received image data and reference image data is greater than an icing threshold.

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